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Single-seat single-engined high-wing monoplane with conventional three-axis control. Wing has unswept leading and trailing edges, and constant chord; cruciform tail. Pitch control by elevator on tail; yaw control by fully flying rudder; roll control by one-third-span ailerons; control inputs through stick for pitch/roll and pedals for yaw. Wing braced from above by kingpost and cables, from below by cables; wing profile; single-surface. Undercarriage has three wheels in tricycle formation with additional tailskid; no suspension on nosewheel and torsion-bar suspension on main wheels. No ground steering. No brakes. Aluminium-tube framework, without pod. Engine mounted below wing driving pusher propeller. Aluminium tubing to US 6061 T6 specification.